Gyrohorizon compass system on a spacecraft

Details Gyrohorizon compass system on a spacecraft Gyrohorizon compass system on a spacecraft

Nov 1981

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981kosis..19..933z&link_type=abstract

Kosmicheskie Issledovaniia, vol. 19, Nov.-Dec. 1981, p. 933-937. In Russian.

Computer Science

Gyrocompasses, Gyroscopic Stability, Spacecraft Instruments, Spacecraft Motion, Equations Of Motion, Gravitational Fields

Scientific paper

Equations of motion are obtained for a gyrohorizon compass system from
the kinetic moment theorem of Blumin and Zavozin (1979). Inequalities
are derived which are the sufficient conditions of the stability of the
gyro system for the case of arbitrary motion of the spacecraft in a
Newtonian gravitational field.

Affiliated with

Also associated with

No associations

Rating

Gyrohorizon compass system on a spacecraft does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Gyrohorizon compass system on a spacecraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gyrohorizon compass system on a spacecraft will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-744476